Airworthiness Directives; Bombardier Model CL600-1A11 (CL-600), Model CL-600-2A12 (CL-601), and Model CL-600-2B16 (CL-601-3A, CL-601- 3R, and CL-604) Series Airplanes, 28988 [C5-9186]
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28988
Corrections
Federal Register
Vol. 70, No. 96
Thursday, May 19, 2005
This section of the FEDERAL REGISTER
contains editorial corrections of previously
published Presidential, Rule, Proposed Rule,
and Notice documents. These corrections are
prepared by the Office of the Federal
Register. Agency prepared corrections are
issued as signed documents and appear in
the appropriate document categories
elsewhere in the issue.
Monday, May 16, 2005, make the
following correction:
On page 26559, in the second column,
following the signature block, the
document line should read ‘‘[FR Doc.
8796 Filed 05–13–05; 8:45 am]’’.
[FR Doc. C5–8796 Filed 5–18–05; 8:45 am]
4. On the same page, in the same
section, in the same table, under the
column Model, in the eighth entry
remove the word ‘‘retraction.’’
[FR Doc. C5–9186 Filed 5–18–05; 8:45 am]
BILLING CODE 1505–01–D
BILLING CODE 1505–01–D
DEPARTMENT OF TRANSPORTATION
DEPARTMENT OF TRANSPORTATION
ENVIRONMENTAL PROTECTION
AGENCY
Federal Aviation Administration
40 CFR Part 52
[R03–OAR–2004–DC–0007; FRL–7909–8]
Approval and Promulgation of Air
Quality Implementation Plans; District
of Columbia; VOC Emission Standards
for AIM Coatings
Correction
In rule document 05–9312 beginning
on page 24959 in the issue of Thursday,
May 12, 2005, make the following
correction:
§52.470
[Corrected]
On pages 24969 and 24970, in
§52.470, in the table, in the column
‘‘EPA approval date’’, ‘‘5/21/05’’ should
read ‘‘5/12/05’’ throughout the column.
[FR Doc. C5–9312 Filed 5–18–05; 8:45 am]
BILLING CODE 1505–01–D
REGULATORY INFORMATION
SERVICE CENTER
Introduction to the Unified Agenda of
Federal Regulatory and Deregulatory
Actions
Correction
In proposed rule document 05–8796
beginning on page 26555 in the issue of
VerDate jul<14>2003
22:18 May 18, 2005
Jkt 205001
14 CFR Part 39
[Docket No. FAA-2005-21139; Directorate
Identifier 2003-NM-196-AD]
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-20356; Directorate
Identifier 2004-NM-115-AD]
RIN 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Bombardier
Model CL600–1A11 (CL–600), Model
CL–600–2A12 (CL–601), and Model CL–
600–2B16 (CL–601–3A, CL–601–3R,
and CL–604) Series Airplanes
Airworthiness Directives; Boeing
Model 737-100, -200, -200C, -300, -400,
and -500 Series Airplanes
Correction
In proposed rule document 05–9186
beginning on page 24331 in the issue of
Monday, May 9, 2005, make the
following corrections:
1. On page 24332, in the table
Messier-Dowty Service Bulletins, under
the column Landing gear component,
the seventh entry should read ‘‘MLG
shock strut pin.’’
2. On the same page, in the same
table, under the column Corresponding
Bombardier service bulletin(s), the
seventh entry should read ‘‘601-0546.’’
In proposed rule document 05–2834
beginning on page 7693 in the issue of
Tuesday, February 15, 2005, make the
following corrections:
§39.13
[Corrected]
3. On page 24334, in §39.13, in Table
2, under the column Messier-Dowty
service bulletin, the last entry should
read ‘‘M-DT SB7300–32–16, dated July
12, 2001.’’.
PO 00000
Frm 00001
Fmt 4734
Sfmt 4734
Correction
§39.13
[Corrected]
1. On page 7695, in the second
column, in §39.13, after amendatory
instruction 2, in the next line, ‘‘FAA–
20356’’ should read ‘‘FAA–2005–
20356.’’
2. On the same page, in the third
column, in the same section, under the
heading Optional Terminating Action,
in the first line, ‘‘(1)’’ should read ‘‘(i).’’
[FR Doc. C5–2834 Filed 5–18–05; 8:45 am]
BILLING CODE 1505–01–D
E:\FR\FM\19MYCX.SGM
19MYCX
]]>Agencies
[Federal Register Volume 70, Number 96 (Thursday, May 19, 2005)]
[Corrections]
[Page 28988]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: C5-9186]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-21139; Directorate Identifier 2003-NM-196-AD]
RIN 2120-AA64
Airworthiness Directives; Bombardier Model CL600-1A11 (CL-600),
Model CL-600-2A12 (CL-601), and Model CL-600-2B16 (CL-601-3A, CL-601-
3R, and CL-604) Series Airplanes
Correction
In proposed rule document 05-9186 beginning on page 24331 in the
issue of Monday, May 9, 2005, make the following corrections:
1. On page 24332, in the table Messier-Dowty Service Bulletins,
under the column Landing gear component, the seventh entry should read
``MLG shock strut pin.''
2. On the same page, in the same table, under the column
Corresponding Bombardier service bulletin(s), the seventh entry should
read ``601-0546.''
Sec. 39.13 [Corrected]
3. On page 24334, in Sec. 39.13, in Table 2, under the column
Messier-Dowty service bulletin, the last entry should read ``M-DT
SB7300-32-16, dated July 12, 2001.''.
4. On the same page, in the same section, in the same table, under
the column Model, in the eighth entry remove the word ``retraction.''
[FR Doc. C5-9186 Filed 5-18-05; 8:45 am]
BILLING CODE 1505-01-D
